# Service difficulty reports: N120UP

A list on [N120UP](https://openairdocs.org/aircraft/N120UP.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 5 · 202 reports

- [SDR IPXA2026092263257](https://openairdocs.org/sdr/IPXA2026092263257.md): Contact · inoperative · Sep 22, 2026 · N120UP · Airbus A300F4622R · Door Warning System
  > SLIDE RELEASE WARNING LIGHT DOES NOT ILLUMINATE DURING TEST, REPLACED CONTACTS IAW ESPM 20-48-25-01. REMOVED AND REPLACED SLIDE RELEASE WARNING LIGHT IAW AMM 52-73-11. OPS CK GOOD.
- [SDR IPXA2026083158089](https://openairdocs.org/sdr/IPXA2026083158089.md): Limit Switch · faulted · Aug 27, 2026 · N120UP · Airbus A300F4622R · Escape Slide
  > AIR TURN BACK, DURING CLIMB THE ESCAPE SLIDE WARNING LIGHT AND ALARM ACTIVATED PASSING THRU 10,000FT. LEVELED OF AT 27,000 FT THEN DESCEND BACK FOR LANDING AND IT CEASED PASSING THRU 14,500 FT. REPLACED EMERGENCY ESCAPE SLIDE SYSTEM LIMIT SWITCHES IAW AMM 52-
- [SDR IPXA2026042054544](https://openairdocs.org/sdr/IPXA2026042054544.md): Light · inoperative · Apr 17, 2026 · N120UP · Airbus A300F4622R · Emergency Lighting
  > LAV EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB OPS CK GOOD REF 33-51-21-02 OK FOR SERVICE
- [SDR IPXA2025041754051](https://openairdocs.org/sdr/IPXA2025041754051.md): Fairing · damaged · Mar 25, 2025 · N120UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > AGING ACFT INSP-300-STR- FUSELAGE SKIN UNDER LEFT LOWER HORIZ STAB FAIRING HAS CHAFE DAMAGE AT AFT SIDE. DOT AA001.FOUND CHAFE DAMAGE THRU CHAFE PLATE 100% MATERIAL LOSS, REMOVED CHAFE PLATE AS REQUIRED IAW SRM 53-19-12 PARA 5.VERIFIED CHAFE DAMAGE THRU CHAFE
- [SDR IPXA2025041754643](https://openairdocs.org/sdr/IPXA2025041754643.md): Fairing · damaged · Mar 25, 2025 · N120UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > AGING ACFT INSP-300-STR- FUSELAGE SKIN UNDER RIGHT LOWER HORIZ STAB FAIRING HAS CHAFE DAMAGE AT AFT SIDE.FOUND CHAFFE DAMAGE TO BE OUT OF LIMITS 100% MATERIAL LOSS. REMOVED CHAFFE PLATE IAW-A300 SRM-53-19-12.PRIMED INTERIOR SIDE IAW-A300-SRM-51-75-10.INSTALLED
- [SDR IPXA2025032554643](https://openairdocs.org/sdr/IPXA2025032554643.md): Skin · chafed · Mar 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN UNDER RIGHT LOWER HORIZ STAB FAIRING HAS CHAFE DAMAGE AT AFT SIDE. [
- [SDR IPXA2025032554051](https://openairdocs.org/sdr/IPXA2025032554051.md): Skin · chafed · Mar 25, 2025 · N120UP · Airbus A300F4622R · Horizontal Stabilizer, Plate/Skin
  > FUSELAGE SKIN UNDER LEFT LOWER HORIZ STAB FAIRING HAS CHAFE DAMAGE AT AFT SIDE.
- [SDR IPXA2025042095015](https://openairdocs.org/sdr/IPXA2025042095015.md): Skin · corroded · Mar 22, 2025 · N120UP · Airbus A300F4622R · Wing, Plate/Skin
  > CONDITION EXIST ON RH WING UPPER SURFACE THAT NEEDS TO BE EVALUATED AT BETWEEN RIB 8 TO RIB10, (SPECIAL ATTENTION AT RIB9).REMOVED PAINT ON RH WING UPPER SURFACE BETWEEN RIB 8 TO RIB 10 AREA BY CHEMICAL METHOD USING PAINT STRIPPER P/N: E3000, BATCH: 4342177, I
- [SDR IPXA2025031998250](https://openairdocs.org/sdr/IPXA2025031998250.md): Adapter · corroded · Mar 17, 2025 · N120UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT ADAPTER AT Y0 RH AT FR 38.2 CORRODED. DOT# 110-401 JP-110.REMOVED CLS ADAPTER AT Y 0 R/H AT FR38.2 IAW A300-600 SRM 51-40-21.INSTALLED ROBBED PART CLS ADAPTER P/N:B53774136200 AT Y0 R/H AT FR38.2 IAW A300-600 SRM 51-40-21. MATERIAL USED SEALANT P/N:04-0
- [SDR IPXA2025031095741](https://openairdocs.org/sdr/IPXA2025031095741.md): Roller · excess play · Mar 6, 2025 · N120UP · Airbus A300F4622R · Passenger/Crew Doors
  > APG-830-CREW DOOR 2 EACH ROLLER ASSYS HAVE EXCESSIVE PLAY DOT# 110-182 JP-110.REMOVED AND REPLACED ROLLER ASSY 2EA IN CREW DOOR IAW AMM 20-21-12.VERIFIED REPLACEMENT OF ROLLER ASSY 2EA IN CREW DOOR IAW AMM 20-21-12.
- [SDR IPXA2025030795741](https://openairdocs.org/sdr/IPXA2025030795741.md): Roller · excess play · Mar 6, 2025 · N120UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR 2 EACH ROLLER ASSYS HAVE EXCESSIVE PLAY. OPE N
- [SDR IPXA2025032115716](https://openairdocs.org/sdr/IPXA2025032115716.md): Web · cracked · Mar 1, 2025 · N120UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > WEB AT FR 69 IS CRACKED FROM -Y300 TO -Y950 AT MANY LOCATIONS DOT# 110-171 JP-110.REMOVED WEB AT FR 69, FROM Y300 TO Y950 AND REMOVED RIVET L/H WEB FOR ACCESS IAW A300 SRM 51-40-21.INSTALLED RIVET L/H WEB AT FR 69 IAW A300 SRM 51-40-21.PERFORMED CUTOUT OF DA
- [SDR IPXA2025031314196](https://openairdocs.org/sdr/IPXA2025031314196.md): Structure · corroded · Mar 1, 2025 · N120UP · Airbus A300F4622R · Leading Edge Devices
  > SDR FILED OPEN, RH WING KRUEGER FLAP NOTED IG CORROSION. INSTALLED RH WING KRUEGER FLAP IAW AMM 27-87-11-0401.
- [SDR IPXA2025040185553](https://openairdocs.org/sdr/IPXA2025040185553.md): Fairing · chafed · Feb 27, 2025 · N120UP · Airbus A300F4622R · Horizontal Stabilizer Structure
  > FAULT-AGING ACFT INSP-300-STR- FUSELAGE SKIN UNDER LEFT LOWER HORIZ STAB FAIRING HAS CHAFE DAMAGE AT AFT SIDE. DOT AA001. VERIFIED INSTALLATION OF LOWER STAB FARING CHAFE PLATE ON LEFT HAND SIDE USING SEALSNT PS870C24 BATCH # 0004366606 AND FAY SEALED WITH 5-
- [SDR IPXA2025031962725](https://openairdocs.org/sdr/IPXA2025031962725.md): Seat Track · corroded · Feb 26, 2025 · N120UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK COMPARTMENT-FLOOR PNL 251LM INSIDE LOWER FR60- C TRACK PLATE HAS CORROSION DOT43-059. ACCOMPLISHED STEP 11, EA#:300-5317-27-A3822, PRELIMINARY 2. "INSTALL CLS ADAPTER PER AIRBUS DRAWING A53275515". USING EXISTING FASTENERS(HI-LOK). COLLAR P/N: NSA
- [SDR IPXA2025031960736](https://openairdocs.org/sdr/IPXA2025031960736.md): Adapter · corroded · Feb 26, 2025 · N120UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK ADAPTER AT FR34, Y0 LEFT EXFOLIATED.. DOT# 110-305 JP-110. ACCOMPLISHED STEP 11, EA #:300-5314-27-A3812, PRELIMINARY 2. "INSTALL CLS ADAPTER PER AIRBUS DRAWING B53774150". ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH UPS EO-92964-REQ1 A
- [SDR IPXA2025031964328](https://openairdocs.org/sdr/IPXA2025031964328.md): Adapter · corroded · Feb 26, 2025 · N120UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK COMPARMENT, FLOOR SUPPORT STRUCTURE, CLS AT PANEL 251LG CORRODED. DOT 28-13. ACCOMPLISHED STEP 3, EA#:300-5316-27-A3814, PRELIMINARY 1." FABRICATE A REPLACEMENT CLS ADAPTER (P/N:A53275451200) PER AIRBUS DRAWING A53275451 FROM MAXIMUM 2.00 INCH THICK
- [SDR IPXA2025040844111](https://openairdocs.org/sdr/IPXA2025040844111.md): Frame · cracked · Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACK FOUND ON HOLE "A" ON FR47 LH HORIZONTAL JUNCTION. AREA MARKED IN BLACK. ERIFIED INSTALLATION OF HAREWARE PER EA 300-5710-27-A3809.COMPLIED WITH EA 300-5710-27-A3809 STEP 31. ACCOMPLISH THE REPAIR PER UPS EO-93045-REQ1 AND EA 300-5710-27-A3809 REV. -.
- [SDR IPXA2025031940161](https://openairdocs.org/sdr/IPXA2025031940161.md): Floor Support · corroded · Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SUPPORT FR11-FR115A, Y1456 CORRODED AT MANY LOCATIONS. DOT# 110-107 JP-110. INSTALLED FLOOR SUPPORT Y1456 LOCATED AT FR11 TO FR19 IAW A300-600F SRM 53-12-15-001-1, SRM 51-40-21-001, DRAWING A53613033210 JH 11000495.
- [SDR IPXA2025031940305](https://openairdocs.org/sdr/IPXA2025031940305.md): Floor Support · corroded · Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SUPPORT CORRODED BETWEEN FR12-FR14, Y1959 DOT# 110-108 JP-110. REMOVE AND REPLACE 1 EACH Y1959 FLOOR SUPPORT (P/N: A53613033212) PER AIRBUS DRAWING A53613033212 REQUIREMENTS AND A300-600F SRM 53-12-15-001-1.
- [SDR IPXA2025032044146](https://openairdocs.org/sdr/IPXA2025032044146.md): Fitting · cracked · Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CRACK FOUND ON HOLE "Q" ON FR47 LH HORIZONTAL JUNCTION. ACCOMPLISHED THE REPAIR PER UPS EO-93045-REQ1 AND EA 300-5710-27-A3809 REV. -.
- [SDR IPXA2025032044127](https://openairdocs.org/sdr/IPXA2025032044127.md): Fitting · cracked · Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CRACK FOUND ON HOLE "P" ON FR47 LH HORIZONTAL JUNCTION. AREA MARKED IN BLACK. ACCOMPLISH THE REPAIR PER UPS EO-93045-REQ1 AND EA 300-5710-27-A3809 REV. -.
- [SDR IPXA2025032044111](https://openairdocs.org/sdr/IPXA2025032044111.md): Frame · cracked · Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACK FOUND ON HOLE "A" ON FR47 LH HORIZONTAL JUNCTION. AREA MARKED IN BLACK. ACCOMPLISH THE REPAIR PER UPS EO-93045-REQ1 AND EA 300-5710-27-A3809 REV. -. C
- [SDR IPXA2025031939728](https://openairdocs.org/sdr/IPXA2025031939728.md): Floor Support · corroded · Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SUPPORT AT FR11-FR15A, Y953 CORRODED AT MANY LOCATIONS. DOT# 110-106 JP-110. INSTALLED FLOOR SUPPORT Y 953 LOCATED AT FR11 TO FR15A IAW A300-600 SRM 51-40-21-001 AND DRAWING A53613033210.
- [SDR IPXA2025022799560](https://openairdocs.org/sdr/IPXA2025022799560.md): Attach Plate · damaged · Feb 22, 2025 · N120UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > FAULT-STR-ZONE 400-#1 ENG PYLON PNL475AL FWD I/B UPPER PLATE HOLE ENLONGATED DOT 43-047. INSTALLED NEW ATTACH FAIRING, IAW A300-600 SRM 51-40-21. USED MATERIAL: SOLID RIVET P/N MS20426AD5-5 BATCH 0004361891. REVIEWED
- [SDR IPXA2025022599592](https://openairdocs.org/sdr/IPXA2025022599592.md): Plate · cracked · Feb 22, 2025 · N120UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > FAULT-STR-ZONE 400-#1 ENG PYLON PNL475AL FWD I/B UPPER PLATE HOLE CRACKED DOT 43-048. INSTALLED NEW ATTACH FAIRING, IAW A300-600 SRM 51-40-21. USED MATERIAL: SOLID RIVET P/N MS20426AD5-5 BATCH 0004361891. REVIEWED
- [SDR IPXA2025040172383](https://openairdocs.org/sdr/IPXA2025040172383.md): Floor Panel · damaged · Feb 21, 2025 · N120UP · Airbus A300F4622R · Fuselage Floor Panel
  > **SUPPLEMENTAL SDR** FAULT-COMP-FUSELAGE TAIL COMPARTMENT FLOOR PANEL BTW FR 84-85 LH SIDE DELAMINATED-DOT 139/34-MR/139. INSTALLED FUSELAGE TAIL COMPARTMENT FLOOR PANEL BTW FR 84-85 LH SIDE I.A.W A300-600 AMM 20-21-12/001. REVIEWED
- [SDR IPXA2025032472383](https://openairdocs.org/sdr/IPXA2025032472383.md): Floor Panel · delaminated · Feb 21, 2025 · N120UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, FUSELAGE TAIL COMPARTMENT FLOOR PANEL BTW FR 84-85 LH SIDE DELAMINATED. CERTIFICATION COMPLETED
- [SDR IPXA2025031385283](https://openairdocs.org/sdr/IPXA2025031385283.md): Rib · damaged · Feb 21, 2025 · N120UP · Airbus A300F4622R · Wing, Rib/Bulkhead
  > DAMAGE INDICATION FOUND INSIDE 2ND LAYER OF FRAME 40 TO CENTER WING JOINT UPPER SKIN LEVEL TENSION BOLT (TOP HOLE) R/H SIDE. ACOMPLISHED REPAIR IN ACCORDANCE WITH UPS EO-93055-REQ1 AND VT-MAE EA 300-5710-27-A3843, REV. -.
- [SDR IPXA2025030786437](https://openairdocs.org/sdr/IPXA2025030786437.md): Rib · cracked · Feb 21, 2025 · N120UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE L/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (3EA) AT RIB LOCATION 26 AFT SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3811, REV.-.
- [SDR IPXA2025030686391](https://openairdocs.org/sdr/IPXA2025030686391.md): Rib · cracked · Feb 21, 2025 · N120UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE L/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 27 FWD SIDE. INSTALL REPAIR DOUBLER GIVEN.COMPLIED WITH STEP 17 OF EA 300-5750-27-A3811. ACCOMPLISH REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3811, REV. -.
- [SDR IPXA2025030786389](https://openairdocs.org/sdr/IPXA2025030786389.md): Rib · cracked · Feb 21, 2025 · N120UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE L/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB LOCATION 27 AFT SIDE. INSTALL REPAIR DOUBLER GIVEN.COMPLIED WITH STEP 17 OF EA 300-5750-27-A3811. ACCOMPLISH REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3811, REV. -.
- [SDR IPXA2025030586446](https://openairdocs.org/sdr/IPXA2025030586446.md): Rib · cracked · Feb 21, 2025 · N120UP · Airbus A300F4622R · Trailing Edge Flaps
  > *SDR FILED OPEN* FAULT: THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 12 AFT SIDE. COMPLIED WITH STEP 17 OF EA 300-5750-27-A3813 PRELIMINARY 1.
- [SDR IPXA2025031161633](https://openairdocs.org/sdr/IPXA2025031161633.md): Bracket · cracked · Feb 20, 2025 · N120UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > E&E BAY FRAME 10 RH WEB BRACKET BROKEN. FABRICATED NEW BRACKET USING MATERIAL 2024-T3.063C, BATCH 0004324652, IAW GMM 09-08, PARAGRAPH 09.08.01.04 AND LOCATED AND DRILLED IAW SRM 51-40-44. INSTALLED NEW BRACKET IAW SRM 51-40-21.
- [SDR IPXA2025020104401](https://openairdocs.org/sdr/IPXA2025020104401.md): Warning Light · inoperative · Jan 31, 2025 · N120UP · Airbus A300F4622R · Door Warning System
  > EVAC SLIDE WARNING LIGHT INOP CLEANED CONNECTOR AT POWER SUPPLY, OPERATIONAL CHECK REF 52-73-11/401. OPERATES NORMALLY. OSD: 2/3/2025
- [SDR IPXA2024091670995](https://openairdocs.org/sdr/IPXA2024091670995.md): Windshield · cracked · Sep 13, 2024 · N120UP · Airbus A300F4622R · Flight Compartment Windows
  > 2:30 INTO FLT@FL340,CAPTS WINDSCREEN OUTER PANE CRACKED LEFT TO RIGHT AT -48 REPLACED L/H WINDSHIELD IAW AMM 56-11-11-0401 OPS CK GOOD.
- [SDR IPXA2024071037812](https://openairdocs.org/sdr/IPXA2024071037812.md): Clamp · loose · Jul 10, 2024 · N120UP · Airbus A300F4622R · Engine Bleed Air System
  > ATB, EMD, PACK #2 ADVISORY FOR HIGH INLET TEMP. NOT ABLE TO CONTROL OR REDUCE TEMP. FOLLOWING TSM 21-61-00 FOUND LARGE BLEED LEAK AT LOOSE CLAMP ON COMPRESSOR BYPASS DUCT ASSY - REPOSITIONED AND TORQUED CLAMP (34H40-400) IAW A300 AMM 21-51-25/401. LEAK CHECK
- [SDR IPXA2023100962149](https://openairdocs.org/sdr/IPXA2023100962149.md): Unknown · unknown · Oct 7, 2023 · N120UP · Airbus A300F4622R · Passenger Compartment Equipment
  > WHILE WORKING WATER INTRUSION DEFERRAL BARCODE T3F18E002SM1Q FOUND FLOOR PANEL 231KJ DAMAGED. MARKED WITH GREEN TAPE.***SM EVAL REQ*** TEMPORARY REPAIR IAW EO-88400-REQ1 DEFERRAL REQUESTED. OPEN
- [SDR IPXA2023092943606](https://openairdocs.org/sdr/IPXA2023092943606.md): Unknown · unknown · Sep 26, 2023 · N120UP · Airbus A300F4622R · Passenger Compartment Equipment
  > OPEN CEILING DAMAGE CENTER COVER PLATE PUNCTURED AND HONEYCOMB DAMAGED AT DOOR POSITION. REF M# 812723 POS AFT CARGO CEILING DOOR ENTRY. REMOVED & REPLACED MM-25-55-10.
- [SDR IPXA2022082785670](https://openairdocs.org/sdr/IPXA2022082785670.md): Bracket · cracked · Aug 27, 2022 · N120UP · Airbus A300* · Trailing Edge Flaps
  > INSPECTION TYPE:1CLH WING FIXED T/E UPPER FAIRING SUPPORT STRUCTURE CRACKED LOCATED ON RIB 10.REMOVED, FABRICATED AND REPLACED PER SRM 51-40-21 AND SRM 57-51-11.
- [SDR IPXA2022082985728](https://openairdocs.org/sdr/IPXA2022082985728.md): None · cracked · Aug 22, 2022 · N120UP · Airbus A300* · Nacelle/Pylon Structure
  > INSPECTION TYPE:SEG#2 ENG PYLON ARC WEB REAR AT BUTTERFLY PANELS HAS CRACKS.WELD REPAIR PER SRM 54-50-00
- [SDR IPXA2022083085765](https://openairdocs.org/sdr/IPXA2022083085765.md): Angle · cracked · Aug 21, 2022 · N120UP · Airbus A300F4622R · Leading Edge Devices
  > INSPECTION TYPE:SEGLH KRUEGER FLAP WELL WEB SUPPORT O/B OF THE ACTUATOR IS CRACKED.REMOVED AND REPLACED PER SRM 51-40-21
- [SDR IPXA2022082985719](https://openairdocs.org/sdr/IPXA2022082985719.md): None · cracked · Aug 21, 2022 · N120UP · Airbus A300* · Nacelle/Pylon Structure
  > INSPECTION TYPE:SEGENG 2 FAIRING 485AL AFT SKIN I/B SIDE WITH 2EA CRACKS.WELD REPAIR PER EO A300-5450-21297-L
- [SDR IPXA2022082985720](https://openairdocs.org/sdr/IPXA2022082985720.md): Precooler · cracked · Aug 20, 2022 · N120UP · Airbus A300* · Nacelle/Pylon Structure
  > INSPECTION TYPE:SEGENG 1 PRECOOLER PANEL 413BL HAS SEVERAL CRACKS.WELD REPAIR PER SRM 54-52-51
- [SDR IPXA2022083185792](https://openairdocs.org/sdr/IPXA2022083185792.md): None · cracked · Aug 19, 2022 · N120UP · Airbus A300* · Emergency Exits
  > INSPECTION TYPE:SEGCLIP CRACKED FOR SUPPORT AT FR 17 E&E COMPARTMENT.REMOVED AND REPLACED PER SRM 51-40-21
- [SDR IPXA2022082985721](https://openairdocs.org/sdr/IPXA2022082985721.md): Precooler · cracked · Aug 19, 2022 · N120UP · Airbus A300* · Nacelle/Pylon Structure
  > INSPECTION TYPE:SEGENG 2 PRECOOLER PANEL 423BL HAS SEVERAL CRACKSWELD REPAIR PER SRM 54-52-51
- [SDR IPXA2022041181064](https://openairdocs.org/sdr/IPXA2022041181064.md): None · dented · Apr 11, 2022 · N120UP · Airbus A300F4622R · Cargo/Baggage Doors
  > INSPECTION TYPE:N/ADENT WITH GOUGE IN AFT BULK CARGO DOOR FORWARD LOWER EDGEREPAIRED AFT BULK CARGO DOOR FORWARD LOWER EDGE IAW E.O A300-5230-83401
- [SDR IPXA2020121763540](https://openairdocs.org/sdr/IPXA2020121763540.md): Door · stuck · Dec 16, 2020 · N120UP · Airbus A300F4622R · Passenger/Crew Doors
  > INSPECTION TYPE: N/A CAPT OPENED MAIN ENTRY DOOR WITH SLIDE LEVER ARMED. THE SLIDE WAS IMMEDIATELY DISARMED AND DID NOT INFLATE BUT THE DOOR WAS STUCK AND WOULD NOT OPEN OR CLOSE. DEPRESSURIZED FWD DOOR DAMPER & EMERGENCY OPERATIONS CYL DEF MAIN CABIN DOOR,
- [SDR IPXA2020050354879](https://openairdocs.org/sdr/IPXA2020050354879.md): Bearing · damaged · May 2, 2020 · N120UP · Airbus A300F4622R · Elevator Structure
  > INSPECTION TYPE:C, AIRCRAFT PITCH BEGAN FEELING HEAVY IN CLIMB. GOT PROGRESSIVE WORSE. APPROCH FLIGHT CONTROLS BEGAN EXTREMLY HEAVY. REMOVED AND REPLACED UPPER BEARING LH #5 RIB BELLCRANK IAW AMM 20-21-12-0001 AND IPC27-31-07-17A ITEM NR 200.
- [SDR IPXA2020042954774](https://openairdocs.org/sdr/IPXA2020042954774.md): Bearing · failed · Apr 28, 2020 · N120UP · Airbus A300F4622R · Elevator Control System
  > EMERGENCY DECLARED, AIRCRAFT PITCH BEGAN FEELING HEAVY IN CLIMB, GOT PROGRESSIVELY WORSE APPROACH FLIGHT CONTROLS BEGAN EXTREMELY HEAVY. UPON SAFE TAXI THE EMERGENCY WAS CANCELLED; NO EQUIP USED. REMOVED AND REPLACED UPPER BEARING ON LT NR 5 RIB BELLCRANK,

Next page: https://openairdocs.org/aircraft/N120UP/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N120UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N120UP/reports

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